Wireless non-radiative energy transfer

ABSTRACT

The electromagnetic energy transfer device includes a first resonator structure receiving energy from an external power supply. The first resonator structure has a first Q-factor. A second resonator structure is positioned distal from the first resonator structure, and supplies useful working power to an external load. The second resonator structure has a second Q-factor. The distance between the two resonators can be larger than the characteristic size of each resonator. Non-radiative energy transfer between the first resonator structure and the second resonator structure is mediated through coupling of their resonant-field evanescent tails.

PRIORITY INFORMATION

This application claims priority from provisional application Ser. No.60/698,442 filed Jul. 12, 2005, which is incorporated herein byreference in its entirety.

STATEMENT AS TO FEDERALLY FUNDED RESEARCH

This invention was made with government support awarded by the NationalScience Foundation under Grant No. DMR-0213282. The government hascertain rights in this invention.

BACKGROUND OF THE INVENTION

The invention relates to the field of oscillatory resonantelectromagnetic modes, and in particular to oscillatory resonantelectromagnetic modes, with localized slowly evanescent field patterns,for wireless non-radiative energy transfer.

In the early days of electromagnetism, before the electrical-wire gridwas deployed, serious interest and effort was devoted towards thedevelopment of schemes to transport energy over long distanceswirelessly, without any carrier medium. These efforts appear to have metwith little, if any, success. Radiative modes of omni-directionalantennas, which work very well for information transfer, are notsuitable for such energy transfer, because a vast majority of energy iswasted into free space. Directed radiation modes, using lasers orhighly-directional antennas, can be efficiently used for energytransfer, even for long distances (transfer distance L_(TRANS)>>L_(DEV),where L_(DEV) is the characteristic size of the device), but requireexistence of an uninterruptible line-of-sight and a complicated trackingsystem in the case of mobile objects.

Rapid development of autonomous electronics of recent years (e.g.laptops, cell-phones, house-hold robots, that all typically rely onchemical energy storage) justifies revisiting investigation of thisissue. Today, the existing electrical-wire grid carries energy almosteverywhere; even a medium-range wireless non-radiative energy transferwould be quite useful. One scheme currently used for some importantapplications relies on induction, but it is restricted to veryclose-range (L_(TRANS)<<L_(DEV)) energy transfers.

SUMMARY OF THE INVENTION

According to one aspect of the invention, there is provided anelectromagnetic energy transfer device. The electromagnetic energytransfer device includes a first resonator structure receiving energyfrom an external power supply. The first resonator structure has a firstQ-factor. A second resonator structure is positioned distal from thefirst resonator structure, and supplies useful working power to anexternal load. The second resonator structure has a second Q-factor. Thedistance between the two resonators can be larger than thecharacteristic size of each resonator. Non-radiative energy transferbetween the first resonator structure and the second resonator structureis mediated through coupling of their resonant-field evanescent tails.

According to another aspect of the invention, there is provided a methodof transferring electromagnetic energy. The method includes providing afirst resonator structure receiving energy from an external powersupply. The first resonator structure has a first Q-factor. Also, themethod includes a second resonator structure being positioned distalfrom the first resonator structure, and supplying useful working powerto an external load. The second resonator structure has a secondQ-factor. The distance between the two resonators can be larger than thecharacteristic size of each resonator. Furthermore, the method includestransferring non-radiative energy between the first resonator structureand the second resonator structure through coupling of theirresonant-field evanescent tails.

In another aspect, an energy transfer method is disclosed including thesteps of providing a first resonator structure receiving energy worn anexternal power supply, said first resonator structure having a firstresonant frequency ω₁, and a first Q-factor Q₁, and characteristic sizeL₁. Providing a second resonator structure being positioned distal fromsaid first resonator structure, at closest distance D, said secondresonator structure having a second resonant frequency ω₁, and a secondQ-factor Q₁, and characteristic size L₂ where the two said frequenciesω₁ and ω₂ are close to within the narrower of the two resonance widthsΓ₁, and Γ₂. Transferring energy non-radiatively between said firstresonator structure and said second resonator structure, said energytransfer being mediated through coupling of their resonant-fieldevanescent tails, and the rate of energy transfer between said firstresonator and said second resonator being denoted by κ, wherenon-radiative means D is smaller than each of the resonant wavelengthsλ₁ and λ₂, where c is the propagation speed of radiation in thesurrounding medium.

Embodiments of the method may include any of the following features. Insome embodiments, said resonators have Q₁>100 and Q₂>100, Q₁>200 andQ₂>200, Q₁>500 and Q₂>500, or even Q₁>1000 and Q₂>1000. In some suchembodiments, κ/sqrt(Γ₁*Γ₂) may be greater than 0.2, greater than 0.5,greater than 1, greater than 2, or even greater than 5. In some suchembodiments D/L₂ may be greater than 1, greater than 2, greater than 3,greater than 5.

In another aspect, an energy transfer device is disclosed whichincludes: a first resonator structure receiving energy from an externalpower supply, said first resonator structure having a first resonantfrequency ω₁, and a first Q-factor Q₁, and characteristic size L₁, and asecond resonator structure being positioned distal from said firstresonator structure, at closest distance D, said second resonatorstructure having a second resonant frequency ω₂, and a second Q-factorQ₂, and characteristic size L₂.

The two said frequencies ω₁ and ω₂ are close to within the narrower ofthe two resonance widths Γ₁, and Γ₂. The non-radiative energy transferbetween said first resonator structure and said second resonatorstructure is mediated through coupling of their resonant-fieldevanescent tails, and the rate of energy transfer between said firstresonator and said second resonator is denoted by κ. The non-radiativemeans D is smaller than each of the resonant wavelengths λ₁ and λ₂,where c is the propagation speed of radiation in the surrounding medium.

Embodiments of the device may include any of the following features. Insome embodiments, said resonators have Q₁>100 and Q₂>100, Q₁>200 andQ₂>200, Q₁>500 and Q₂>500, or even Q₁>1000 and Q₂>1000. In some suchembodiments, κ/sqrt(Γ₁*Γ₂) may be greater than 0.2, greater than 0.5,greater than 1, greater than 2, or even greater than 5. In some suchembodiments D/L₂ may be greater than 1, greater than 2, greater than 3,or even greater than 5.

In some embodiments, the resonant field in the device iselectromagnetic.

In some embodiments, the first resonator structure includes a dielectricsphere, where the characteristic size L₁ is the radius of the sphere.

In some embodiments, the first resonator structure includes a metallicsphere, where the characteristic size L₁ is the radius of the sphere.

In some embodiments, the first resonator structure includes ametallodielectric sphere, where the characteristic size L₁ is the radiusof the sphere.

In some embodiments, the first resonator structure includes a plasmonicsphere, where the characteristic size L₁ is the radius of the sphere.

In some embodiments, the first resonator structure includes apolaritonic sphere, where the characteristic size L₁ is the radius ofthe sphere.

In some embodiments, the first resonator structure includes acapacitively-loaded conducting-wire loop, where the characteristic sizeL₁ is the radius of the loop.

In some embodiments, the second resonator structure includes adielectric sphere, where the characteristic size L₂ is the radius of thesphere.

In some embodiments, the second resonator structure includes a metallicsphere where the characteristic size L₂ is the radius of the sphere.

In some embodiments, the second resonator structure includes ametallodielectric sphere where the characteristic, size L₂ is the radiusof the sphere.

In some embodiments, the second resonator structure includes a plasmonicsphere where the characteristic size L₂ is the radius of the sphere.

In some embodiments, the second resonator structure includes apolaritonic sphere where the characteristic size L₂ is the radius of thesphere.

In some embodiments, the second resonator structure includes acapacitively-loaded conducting-wire loop where the characteristic sizeL₂ is the radius of the loop.

In some embodiments, the resonant field in the device is acoustic.

It is to be understood that embodiments of the above described methodsand devices may include any of the above listed features, alone or incombination.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a schematic diagram illustrating an exemplary embodiment ofthe invention;

FIG. 2A is a numerical FDTD result for a high-index disk cavity ofradius r along with the electric field; FIG. 2B a numerical FDTD resultfor a medium-distance coupling between two resonant disk cavities:initially, all the energy is in one cavity (left panel); after some timeboth cavities are equally excited (right panel).

FIG. 3 is schematic diagram demonstrating two capacitively-loadedconducting-wire loops;

FIGS. 4A-4B are numerical FDTD results for reduction in radiation-Q ofthe resonant disk cavity due to scattering from extraneous objects;

FIG. 5 is a numerical FDTD result for medium-distance coupling betweentwo resonant disk cavities in the presence of extraneous objects; and

FIGS. 6A-6B are graphs demonstrating efficiencies of converting thesupplied power into useful work (η_(w)), radiation and ohmic loss at thedevice (η_(d)), and the source (η_(s)), and dissipation inside a human(η_(h)), as a function of the coupling-to-loss ratio κ/Γ_(d); in panel(a) Γ_(w) is chosen so as to minimize the energy stored in the device,while in panel (b) Γ_(w) is chosen so as to maximize the efficiency ηwfor each κ/Γ_(d).

DETAILED DESCRIPTION OF THE INVENTION

In contrast to the currently existing schemes, the invention providesthe feasibility of using long-lived oscillatory resonant electromagneticmodes, with localized slowly evanescent field patterns, for wirelessnon-radiative energy transfer. The basis of this technique is that twosame-frequency resonant objects tend to couple, while interacting weaklywith other off-resonant environmental objects. The purpose of theinvention is to quantify this mechanism using specific examples, namelyquantitatively address the following questions: up to which distancescan such a scheme be efficient and how sensitive is it to externalperturbations. Detailed theoretical and numerical analysis show that amid-range (L_(TRANS)≈few*L_(DEV)) wireless energy-exchange can actuallybe achieved, while suffering only modest transfer and dissipation ofenergy into other off-resonant objects.

The omnidirectional but stationary (non-lossy) nature of the near fieldmakes this mechanism suitable for mobile wireless receivers. It couldtherefore have a variety of possible applications including for example,placing a source connected to the wired electricity network on theceiling of a factory room, while devices, such as robots, vehicles,computers, or similar, are roaming freely within the room. Otherpossible applications include electric-engine buses, RFIDs, and perhapseven nano-robots.

The range and rate of the inventive wireless energy-transfer scheme arethe first subjects of examination, without considering yet energydrainage from the system for use into work. An appropriate analyticalframework for modeling the exchange of energy between resonant objectsis a weak-coupling approach called “coupled-mode theory”. FIG. 1 is aschematic diagram illustrating a general description of the invention.The invention uses a source and device to perform energy transferring.Both the source 1 and device 2 are resonator structures, and areseparated a distance D from each other. In this arrangement, theelectromagnetic field of the system of source 1 and device 2 isapproximated by F(r,t)≈a₁(t)F₁(r)+a₂(t)F₂(r), whereF_(1,2)(r)=[E_(1,2)(r) H_(1,2)(r)] are the eigenmodes of source 1 anddevice 2 alone, and then the field amplitudes a₁(t) and a₂(t) can beshown to satisfy the “coupled-mode theory”:

$\begin{matrix}{{{\frac{\mathbb{d}a_{1}}{\mathbb{d}t} = {{{- {{\mathbb{i}}\left( {\omega_{1} - {\mathbb{i}\Gamma}_{1}} \right)}}a_{1}} + {{\mathbb{i}\kappa}_{11}a_{1}} + {{\mathbb{i}\kappa}_{12}a_{2}}}}\frac{\mathbb{d}a_{2}}{\mathbb{d}t} = {{{- {{\mathbb{i}}\left( {\omega_{2} - {\mathbb{i}\Gamma}_{2}} \right)}}a_{2}} + {{\mathbb{i}\kappa}_{22}a_{2}} + {{\mathbb{i}\kappa}_{21}a_{1}}}},} & (1)\end{matrix}$where ω_(1,2) are the individual eigen-frequencies, Γ_(1,2) are theresonance widths due to the objects' intrinsic (absorption, radiationetc.) losses, κ_(12,21) are the coupling coefficients, and κ_(11,22)model the shift in the complex frequency of each object due to thepresence of the other.

The approach of Eq. 1 has been shown, on numerous occasions, to providean excellent description of resonant phenomena for objects of similarcomplex eigen-frequencies (namely |ω₁−ω₂|<<|κ_(12,21)| and Γ₁≈Γ₂), whoseresonances are reasonably well defined (namelyΓ_(1,2)&Im{κ_(11,22)}<<|κ_(12,21)|) and in the weak coupling limit(namely |K_(1,2)|<<ω_(1,2)). Coincidentally, these requirements alsoenable optimal operation for energy transfer. Also, Eq. (1) show thatthe energy exchange can be nearly perfect at exact resonance (ω₁=ω₂ andΓ₁=Γ₂), and that the losses are minimal when the “coupling-time” is muchshorter than all “loss-times”. Therefore, the invention requiresresonant modes of high Q=ω/(2Γ) for low intrinsic-loss rates Γ_(1,2),and with evanescent tails significantly longer than the characteristicsizes L₁ and L₂ of the two objects for strong coupling rate |K_(12,21)|over large distances D, where D is the closest distance between the twoobjects. This is a regime of operation that has not been studiedextensively, since one usually prefers short tails, to minimizeinterference with nearby devices.

Objects of nearly infinite extent, such as dielectric waveguides, cansupport guided modes whose evanescent tails are decaying exponentiallyin the direction away from the object, slowly if tuned close to cutoff,and can have nearly infinite Q. To implement the inventiveenergy-transfer scheme, such geometries might be suitable for certainapplications, but usually finite objects, namely ones that aretopologically surrounded everywhere by air, are more appropriate.

Unfortunately, objects of finite extent cannot support electromagneticstates that are exponentially decaying in all directions in air, sincein free space: {right arrow over (k)}²=ω²/c². Because of this, one canshow that they cannot support states of infinite Q. However, verylong-lived (so-called “high-Q”) states can be found, whose tails displaythe needed exponential-like decay away from the resonant object overlong enough distances before they turn oscillatory (radiative). Thelimiting surface, where this change in the field behavior happens, iscalled the “radiation caustic”, and, for the wireless energy-transferscheme to be based on the near field rather than the far/radiationfield, the distance between the coupled objects must be such that onelies within the radiation caustic of the other.

The invention is very general and any type of resonant structuresatisfying the above requirements can be used for its implementation. Asexamples and for definiteness, one can choose to work with twowell-known, but quite different electromagnetic resonant systems:dielectric disks and capacitively-loaded conducting-wire loops. Evenwithout optimization, and despite their simplicity, both will be shownto exhibit fairly good performance. Their difference lies mostly in thefrequency range of applicability due to practical considerations, forexample, in the optical regime dielectrics prevail, since conductivematerials are highly lossy.

Consider a 2D dielectric disk cavity of radius r and permittivity ∈surrounded by air that supports high-Q whispering-gallery modes, asshown in FIG. 2A. Such a cavity is studied using both analyticalmodeling, such as separation of variables in cylindrical coordinates andapplication of boundary conditions, and detailed numericalfinite-difference-time-domain (FDTD) simulations with a resolution of 30pts/r. Note that the physics of the 3D case should not be significantlydifferent, while the analytical complexity and numerical requirementswould be immensely increased. The results of the two methods for thecomplex eigen-frequencies and the field patterns of the so-called“leaky” eigenmodes are in an excellent agreement with each other for avariety of geometries and parameters of interest.

The radial modal decay length, which determines the coupling strengthκ≡|κ₂₁|=κ₁₂|, is on the order of the wavelength, therefore, fornear-field coupling to take place between cavities whose distance ismuch larger than their size, one needs subwavelength-sized resonantobjects (r<<λ). High-radiation-Q and long-tailed subwavelengthresonances can be achieved, when the dielectric permittivity ∈ is aslarge as practically possible and the azimuthal field variations (ofprincipal number m) are slow (namely m is small).

One such TE-polarized dielectric-cavity mode, which has the favorablecharacteristics Q_(rad)=1992 and λ/r=20 using ∈=147.7 and m=2, is shownin FIG. 2A, and will be the “test” cavity 18 for all subsequentcalculations for this class of resonant objects. Another example of asuitable cavity has Q_(rad)=9100 and λ/r=10 using ∈=65.61 and m=3. Thesevalues of ∈ might at first seem unrealistically large. However, not onlyare there in the microwave regime (appropriate for meter-range couplingapplications) many materials that have both reasonably high enoughdielectric constants and low losses, for example, Titania: ∈≈96,Im{∈}/∈≈10⁻³; Barium tetratitanate: ∈≈37, Im{∈}/∈≈10⁻⁴; Lithiumtantalite: ∈≈40, Im{∈}/∈≈10⁻⁴; etc.), but also ∈ could instead signifythe effective index of other known subwavelength (λ/r>>1) surface-wavesystems, such as surface-plasmon modes on surfaces of metal-like(negative-∈) materials or metallodielectric photonic crystals.

With regards to material absorption, typical loss tangents in themicrowave (e.g. those listed for the materials above) suggest thatQ_(abs)˜∈/Im{∈}˜10000. Combining the effects of radiation andabsorption, the above analysis implies that for a properly designedresonant device-object d a value of Q_(d)˜2000 should be achievable.Note though, that the resonant source s will in practice often beimmobile, and the restrictions on its allowed geometry and size willtypically be much less stringent than the restrictions on the design ofthe device; therefore, it is reasonable to assume that the radiativelosses can be designed to be negligible allowing for Q_(s)˜10000,limited only by absorption.

To calculate now the achievable rate of energy transfer, one can placetwo of the cavities 20, 22 at distance D between their centers, as shownin FIG. 2B. The normal modes of the combined system are then an even andan odd superposition of the initial modes and their frequencies aresplit by the coupling coefficient κ, which we want to calculate.Analytically, coupled-mode theory gives for dielectric objectsκ₁₂=ω₂/2·∫d³rE*₁(r)E₂(r)∈₁(r)/∫d³r|E₁(r)|²∈(r), where ∈_(1,2)(r) denotethe dielectric functions of only object 1 alone or 2 alone excluding thebackground dielectric (free space) and ∈(r) the dielectric function ofthe entire space with both objects present. Numerically, one can find κusing FDTD simulations either by exciting one of the cavities andcalculating the energy-transfer time to the other or by determining thesplit normal-mode frequencies. For the “test” disk cavity the radiusr_(C) of the radiation caustic is r_(C)≈11r, and for non-radiativecoupling D<r_(C), therefore here one can choose D/r=10, 7, 5, 3. Then,for the mode of FIG. 3, which is odd with respect to the line thatconnects the two cavities, the analytical predictions are ω/2κ=1602,771, 298, 48, while the numerical predictions are ω/2κ=1717, 770, 298,47 respectively, so the two methods agree well. The radiation fields ofthe two initial cavity modes interfere constructively or destructivelydepending on their relative phases and amplitudes, leading to increasedor decreased net radiation loss respectively, therefore for any cavitydistance the even and odd normal modes have Qs that are one larger andone smaller than the initial single-cavity Q=1992 (a phenomenon notcaptured by coupled-mode theory), but in a way that the average Γ isalways approximately Γ≈ω/2Q. Therefore, the correspondingcoupling-to-loss ratios are κ/Γ=1.16, 2.59, 6.68, 42.49, and althoughthey do not fall in the ideal operating regime κ/Γ>>1, the achievedvalues are still large enough to be useful for applications.

Consider a loop 10 or 12 of N coils of radius r of conducting wire withcircular cross-section of radius a surrounded by air, as shown in FIG.3. This wire has inductance L=μ_(o)N²r[ln(8r/α)−2], where μ_(o) is themagnetic permeability of free space, so connecting it to a capacitance Cwill make the loop resonant at frequency ω=1/√{square root over (LC)}.The nature of the resonance lies in the periodic exchange of energy fromthe electric field inside the capacitor due to the voltage across it tothe magnetic field in free space due to the current in the wire. Lossesin this resonant system consist of ohmic loss inside the wire andradiative loss into free space.

For non-radiative coupling one should use the near-field region, whoseextent is set roughly by the wavelength λ, therefore the preferableoperating regime is that where the loop is small (r<<λ). In this limit,the resistances associated with the two loss channels are respectivelyR_(ohm)=√{square root over (μ_(o)ρω/2)}·Nr/α andR_(rad)=π/6·η_(o)N²(ωr/c)⁴, where ρ is the resistivity of the wirematerial and η_(o)≈120πΩ is the impedance of free space. The qualityfactor of such a resonance is then Q=ωL/(R_(ohm)+R_(rad)) and is highestfor some frequency determined by the system parameters: at lowerfrequencies it is dominated by ohmic loss and at higher frequencies byradiation.

To get a rough estimate in the microwave, one can use one coil (N=1) ofcopper ρ=1.69·10⁻⁸ Ωm) wire and then for r=1 cm and α=1 mm, appropriatefor example for a cell phone, the quality factor peaks to Q=1225 atf=380 MHz, for r=30 cm and α=2 mm for a laptop or a household robotQ=1103 at f=17 MHz, while for r=1 m and α=4 mm (that could be a sourceloop on a room ceiling) Q=1315 at f=5 MHz. So in general, expectedquality factors are Q≈1000-1500 at λ/r≈50-80, namely suitable fornear-field coupling.

The rate for energy transfer between two loops 10 and 12 at distance Dbetween their centers, as shown in FIG. 3, is given by κ₁₂=ωM/2√{squareroot over (L₁L₂)}, where M is the mutual inductance of the two loops 10and 12. In the limit r<<D<<λ one can use the quasi-static resultM=π/4·μ_(o)N₁N₂(r₁r₂)²/D³, which means that ω/2κ˜(D/√{square root over(r₁r₂)})³. For example, by choosing again D/r=10, 8, 6 one can get fortwo loops of r=1 cm, same as used before, that ω/2κ=3033, 1553, 655respectively, for the r=30 cm that ω/2κ=7131, 3651, 1540, and for ther=1 m that ω/2κ=6481, 3318, 1400. The corresponding coupling-to-lossratios peak at the frequency where peaks the single-loop Q and areκ/Γ=0.4, 0.79, 1.97 and 0.15, 0.3, 0.72 and 0.2, 0.4, 0.94 for the threeloop-kinds and distances. An example of dissimilar loops is that of ar=1 m (source on the ceiling) loop and a r=30 cm (household robot on thefloor) loop at a distance D=3 m (room height) apart, for whichκ/√{square root over (Γ₁Γ₂)}=0.88 peaks at f=6.4 MHz, in between thepeaks of the individual Q's. Again, these values are not in the optimalregime κ/Γ>>1, but will be shown to be sufficient.

It is important to appreciate the difference between this inductivescheme and the already used close-range inductive schemes for energytransfer in that those schemes are non-resonant. Using coupled-modetheory it is easy to show that, keeping the geometry and the energystored at the source fixed, the presently proposed resonant-couplinginductive mechanism allows for Q approximately 1000 times more powerdelivered for work at the device than the traditional non-resonantmechanism, and this is why mid-range energy transfer is now possible.Capacitively-loaded conductive loops are actually being widely used asresonant antennas (for example in cell phones), but those operate in thefar-field regime with r/λ˜1, and the radiation Q's are intentionallydesigned to be small to make the antenna efficient, so they are notappropriate for energy transfer.

Clearly, the success of the inventive resonance-based wirelessenergy-transfer scheme depends strongly on the robustness of theobjects' resonances. Therefore, their sensitivity to the near presenceof random non-resonant extraneous objects is another aspect of theproposed scheme that requires analysis. The interaction of an extraneousobject with a resonant object can be obtained by a modification of thecoupled-mode-theory model in Eq. (1), since the extraneous object eitherdoes not have a well-defined resonance or is far-off-resonance, theenergy exchange between the resonant and extraneous objects is minimal,so the term κ₁₂ in Eq. (1) can be dropped. The appropriate analyticalmodel for the field amplitude in the resonant object α₁(t) becomes:

$\begin{matrix}{\frac{\mathbb{d}a_{1}}{\mathbb{d}t} = {{{- {{\mathbb{i}}\left( {\omega_{1} - {\mathbb{i}\Gamma}_{1}} \right)}}a_{1}} + {{\mathbb{i}\kappa}_{11}a_{1}}}} & (2)\end{matrix}$

Namely, the effect of the extraneous object is just a perturbation onthe resonance of the resonant object and it is twofold: First, it shiftsits resonant frequency through the real part of κ₁₁ thus detuning itfrom other resonant objects. This is a problem that can be fixed rathereasily by applying a feedback mechanism to every device that correctsits frequency, such as through small changes in geometry, and matches itto that of the source. Second, it forces the resonant object to losemodal energy due to scattering into radiation from the extraneous objectthrough the induced polarization or currents in it, and due to materialabsorption in the extraneous object through the imaginary part of κ₁₁.This reduction in Q can be a detrimental effect to the functionality ofthe energy-transfer scheme, because it cannot be remedied, so itsmagnitude must be quantified.

In the first example of resonant objects that have been considered, theclass of dielectric disks, small, low-index, low-material-loss orfar-away stray objects will induce small scattering and absorption. Toexamine realistic cases that are more dangerous for reduction in Q, onecan therefore place the “test” dielectric disk cavity 40 close to: a)another off-resonance object 42, such as a human being, of largeRe{∈}=49 and Im{∈}=16 and of same size but different shape, as shown inFIG. 4A; and b) a roughened surface 46, such as a wall, of large extentbut of small Re{∈}=2.5 and Im{∈}=0.05, as shown in FIG. 4B.

Analytically, for objects that interact with a small perturbation thereduced value of radiation-Q due to scattering could be estimated usingthe polarization ∫d³r|P_(X1)(r)|²∝∫d³r|E₁(r)·Re{∈_(X)(r)}|² induced bythe resonant cavity 1 inside the extraneous object X=42 or roughenedsurface X=46. Since in the examined cases either the refractive index orthe size of the extraneous objects is large, these first-orderperturbation-theory results would not be accurate enough, thus one canonly rely on numerical FDTD simulations. The absorption-Q inside theseobjects can be estimated throughIm{κ₁₁}=ω₁/2·∫d³r|E₁(r)|²Im{∈_(X)(r)}/∫d³r|E₁(r)|²∈(r).

Using these methods, for distances D/r=10, 7, 5, 3 between the cavityand extraneous-object centers one can find that Q_(rad)=1992 isrespectively reduced to Q_(rad)=1988, 1258, 702, 226, and that theabsorption rate inside the object is Q_(abs)=312530, 86980, 21864, 1662,namely the resonance of the cavity is not detrimentally disturbed fromhigh-index and/or high-loss extraneous objects, unless the (possiblymobile) object comes very close to the cavity. For distances D/r=10, 7,5, 3, 0 of the cavity to the roughened surface we find respectivelyQ_(rad)=2101, 2257, 1760, 1110, 572, and Q_(abs)>4000, namely theinfluence on the initial resonant mode is acceptably low, even in theextreme case when the cavity is embedded on the surface. Note that aclose proximity of metallic objects could also significantly scatter theresonant field, but one can assume for simplicity that such objects arenot present.

Imagine now a combined system where a resonant source-object s is usedto wirelessly transfer energy to a resonant device-object d but there isan off-resonance extraneous-object e present. One can see that thestrength of all extrinsic loss mechanisms from e is determined by|E_(s)(r_(e))|², by the square of the small amplitude of the tails ofthe resonant source, evaluated at the position r_(e) of the extraneousobject. In contrast, the coefficient of resonant coupling of energy fromthe source to the device is determined by the same-order tail amplitude|E_(s)(r_(d))|, evaluated at the position r_(d) of the device, but thistime it is not squared! Therefore, for equal distances of the source tothe device and to the extraneous object, the coupling time for energyexchange with the device is much shorter than the time needed for thelosses inside the extraneous object to accumulate, especially if theamplitude of the resonant field has an exponential-like decay away fromthe source. One could actually optimize the performance by designing thesystem so that the desired coupling is achieved with smaller tails atthe source and longer at the device, so that interference to the sourcefrom the other objects is minimal.

The above concepts can be verified in the case of dielectric diskcavities by a simulation that combines FIGS. 2A-2B and 4A-4B, namelythat of two (source-device) “test” cavities 50 placed 10r apart, in thepresence of a same-size extraneous object 52 of ∈=49 between them, andat a distance 5r from a large roughened surface 56 of ∈=2.5, as shown inFIG. 5. Then, the original values of Q=1992, ω/2κ=1717 (and thusκ/Γ=1.16) deteriorate to Q=765, ω/2κ=965 (and thus κ/Γ=0.79). Thischange is acceptably small, considering the extent of the consideredexternal perturbation, and, since the system design has not beenoptimized, the final value of coupling-to-loss ratio is promising thatthis scheme can be useful for energy transfer.

In the second example of resonant objects being considered, theconducting-wire loops, the influence of extraneous objects on theresonances is nearly absent. The reason for this is that, in thequasi-static regime of operation (r<<λ) that is being considered, thenear field in the air region surrounding the loop is predominantlymagnetic, since the electric field is localized inside the capacitor.Therefore, extraneous objects that could interact with this field andact as a perturbation to the resonance are those having significantmagnetic properties (magnetic permeability Re{μ}>1 or magnetic lossIm{μ}>0). Since almost all common materials are non-magnetic, theyrespond to magnetic fields in the same way as free space, and thus willnot disturb the resonance of a conducting-wire loop. The onlyperturbation that is expected to affect these resonances is a closeproximity of large metallic structures.

An extremely important implication of the above fact relates to safetyconsiderations for human beings. Humans are also non-magnetic and cansustain strong magnetic fields without undergoing any risk. This isclearly an advantage of this class of resonant systems for manyreal-world applications. On the other hand, dielectric systems of high(effective) index have the advantages that their efficiencies seem to behigher, judging from the larger achieved values of κ/Γ, and that theyare also applicable to much smaller length-scales, as mentioned before.

Consider now again the combined system of resonant source s and device din the presence of a human h and a wall, and now let us study theefficiency of this resonance-based energy-transfer scheme, when energyis being drained from the device for use into operational work. One canuse the parameters found before: for dielectric disks,absorption-dominated loss at the source Q_(s)˜10⁴, radiation-dominatedloss at the device Q_(d)˜10³ (which includes scattering from the humanand the wall), absorption of the source- and device-energy at the humanQ_(s-h), Q_(d-h)˜10⁴−10⁵ depending on his/her not-very-close distancefrom the objects, and negligible absorption loss in the wall; forconducting-wire loops, Q_(s)˜Q_(d)˜10³, and perturbations from the humanand the wall are negligible. With corresponding loss-rates Γ=ω/2Q,distance-dependent coupling κ, and the rate at which working power isextracted Γ_(w), the coupled-mode-theory equation for the devicefield-amplitude is

$\begin{matrix}{\frac{\mathbb{d}a_{d}}{\mathbb{d}t} = {{{- {{\mathbb{i}}\left( {\omega - {\mathbb{i}\Gamma}_{d}} \right)}}a_{d}} + {{\mathbb{i}\kappa}\; a_{s}} - {\Gamma_{d - h}a_{d}} - {\Gamma_{w}{a_{d}.}}}} & (3)\end{matrix}$

Different temporal schemes can be used to extract power from the deviceand their efficiencies exhibit different dependence on the combinedsystem parameters. Here, one can assume steady state, such that thefield amplitude inside the source is maintained constant, namelyα_(s)(t)=A_(s)e^(−iωt), so then the field amplitude inside the device isα_(d)(t)=A_(d)e^(−iωt) with A_(d)=iκ/(Γ_(d)+Γ_(d-h)+Γ_(w))A_(s).Therefore, the power lost at the source is P_(s)=2Γ_(s)|A_(s)|², at thedevice it is P_(d)=2Γ_(d)|A_(d)|², the power absorbed at the human isP_(h)=2Γ_(s-h)|A_(s)|²+2Γ_(d-h)|A_(d)|², and the useful extracted poweris P_(w)=2Γ_(w)|A_(d)|². From energy conservation, the total powerentering the system is P_(total)=P_(s)+P_(d)+P_(h)+P_(w). Denote thetotal loss-rates Γ_(s) ^(tot)=Γ_(s)+Γ_(s-h) and Γ_(d)^(tot)=Γ_(d)+Γ_(d-h). Depending on the targeted application, thework-drainage rate should be chosen either Γ_(w)=Γ_(d) ^(tot) tominimize the required energy stored in the resonant objects orΓ_(w)=Γ_(d) ^(tot)√{square root over (1+κ²/Γ_(s) ^(tot)Γ_(d)^(tot))}>Γ_(d) ^(tot) such that the ratio of useful-to-lost powersnamely the efficiency η_(w)=P_(w)/P_(total), is maximized for some valueof κ. The efficiencies η for the two different choices are shown inFIGS. 6A and 6B respectively, as a function of the κ/Γ_(d)figure-of-merit which in turn depends on the source-device distance.

FIGS. 6A-6B show that for the system of dielectric disks and the choiceof optimized efficiency, the efficiency can be large, e.g., at least40%. The dissipation of energy inside the human is small enough, lessthan 5%, for values κ/Γ_(d)>1 and Q_(h)>10⁵, namely for medium-rangesource-device distances (D_(d)/r<10) and most human-source/devicedistances (D_(h)/r>8). For example, for D_(d)/r=10 and D_(h)/r=8, if 10W must be delivered to the load, then, from FIG. 6B, ˜0.4 W will bedissipated inside the human, ˜4 W will be absorbed inside the source,and ˜2.6 W will be radiated to free space. For the system ofconducting-wire loops, the achieved efficiency is smaller, ˜20% forκ/Γ_(d)≈1, but the significant advantage is that there is no dissipationof energy inside the human, as explained earlier.

Even better performance should be achievable through optimization of theresonant object designs. Also, by exploiting the earlier mentionedinterference effects between the radiation fields of the coupledobjects, such as continuous-wave operation at the frequency of thenormal mode that has the larger radiation-Q, one could further improvethe overall system functionality. Thus the inventive wirelessenergy-transfer scheme is promising for many modern applications.Although all considerations have been for a static geometry, all theresults can be applied directly for the dynamic geometries of mobileobjects, since the energy-transfer time κ⁻¹˜1 μs, which is much shorterthan any timescale associated with motions of macroscopic objects.

The invention provides a resonance-based scheme for mid-range wirelessnon-radiative energy transfer. Analyses of very simple implementationgeometries provide encouraging performance characteristics for thepotential applicability of the proposed mechanism. For example, in themacroscopic world, this scheme could be used to deliver power to robotsand/or computers in a factory room, or electric buses on a highway(source-cavity would in this case be a “pipe” running above thehighway). In the microscopic world, where much smaller wavelengths wouldbe used and smaller powers are needed, one could use it to implementoptical inter-connects for CMOS electronics or else to transfer energyto autonomous nano-objects, without worrying much about the relativealignment between the sources and the devices; energy-transfer distancecould be even longer compared to the objects' size, since Im{∈(ω)} ofdielectric materials can be much lower at the required opticalfrequencies than it is at microwave frequencies.

As a venue of future scientific research, different material systemsshould be investigated for enhanced performance or different range ofapplicability. For example, it might be possible to significantlyimprove performance by exploring plasmonic systems. These systems canoften have spatial variations of fields on their surface that are muchshorter than the free-space wavelength, and it is precisely this featurethat enables the required decoupling of the scales: the resonant objectcan be significantly smaller than the exponential-like tails of itsfield. Furthermore, one should also investigate using acousticresonances for applications in which source and device are connected viaa common condensed-matter object.

Although the present invention has been shown and described with respectto several preferred embodiments thereof, various changes, omissions andadditions to the form and detail thereof, may be made therein, withoutdeparting from the spirit and scope of the invention.

1. A method of transferring electromagnetic energy comprising: providinga first electromagnetic resonator structure receiving energy from anexternal power supply, said first resonator structure having a firstmode with a resonant frequency ω₁, an intrinsic loss rate Γ₁, and afirst Q-factor Q₁=ω₁/(2Γ₁), providing a second electromagnetic resonatorstructure being positioned distal from said first resonator structureand not electrically wired to the first resonator structure, said secondresonator structure having a second mode with a resonant frequency ω₂,an intrinsic loss rate Γ₂, and a second Q-factor Q₂=ω₂/(2Γ₂),transferring electromagnetic energy from said first resonator structureto said second resonator structure over a distance D that is smallerthan each of the resonant wavelengths λ₁ and λ₂ corresponding to theresonant frequencies ω₁ and ω₂, respectively, wherein theelectromagnetic resonator structures are designed to have Q₁>100 andQ₂>100.
 2. The method of claim 1, wherein the two said frequencies ω₁and ω₂ are close to within the narrower of Γ₁, and Γ₂.
 3. The method ofclaim 1, wherein Q₁>200, and Q₂>200.
 4. The method of claim 1, whereinQ₁>500, and Q₂>500.
 5. The method of claim 1, wherein Q₁>1000, andQ₂>1000.
 6. An electromagnetic energy transfer system comprising: afirst electromagnetic resonator structure receiving energy from anexternal power supply, said first resonator structure having a firstmode with a resonant frequency ω₁, an intrinsic loss rate Γ₁, and afirst Q-factor Q₁ω₁/(2Γ₁), and a second electromagnetic resonatorstructure being positioned distal from said first resonator structureand not electrically wired to the first resonator structure, said secondresonator structure having a second mode having a resonant frequency ω₂,said second resonator structure having a second mode with a resonantfrequency ω₂, an intrinsic loss rate Γ₂, and a second Q-factorQ₂=ω₂/(2Γ₂), wherein said first resonator transfers electromagneticenergy to said second resonator over a distance D that is smaller thaneach of the resonant wavelengths λ₁ and λ₂ corresponding to the resonantfrequencies w₁ and ω₂, respectively, wherein the electromagneticresonator structures are designed to have Q₁>100 and Q₂>100.
 7. Theenergy transfer system of claim 6, wherein Q₁>200, and Q₂>200.
 8. Theenergy transfer system of claim 6, wherein said first resonatorstructure comprises a dielectric sphere having a radius defining acharacteristic size L₁ for the first resonator structure.
 9. The energytransfer system of claim 6, wherein said first resonator structurecomprises a metallic sphere having a radius defining a characteristicsize L₁ for the first resonator structure.
 10. The energy transfersystem of claim 6, and wherein said first resonator structure comprisesa metallodielectric sphere having a radius defining a characteristicsize L₁ for the first resonator structure.
 11. The energy transfersystem of claim 6, wherein said first resonator structure comprises aplasmonic sphere having a radius defining a characteristic size L₁ forthe first resonator structure.
 12. The energy transfer system of claim6, wherein said first resonator structure comprises a polaritonic spherehaving a radius defining a characteristic size L₁ for the firstresonator structure.
 13. The energy transfer device of claim 6, and saidfirst resonator structure comprises a capacitively-loadedconducting-wire loop, where the radius of the loop defines acharacteristic size L₁ for the first resonator structure.
 14. The energytransfer system of claim 6, and said second resonator structurecomprises a dielectric sphere, having a radius defining a characteristicsize L₂ for the second resonator structure.
 15. The energy transfersystem of claim 6, and said second resonator structure comprises ametallic sphere, having a radius defining a characteristic size L₂ forthe second resonator structure.
 16. The energy transfer system of claim6, and said second resonator structure comprises a metallodielectricsphere, having a radius defining a characteristic size L₂ for the secondresonator structure.
 17. The energy transfer system of claim 6, and saidsecond resonator structure comprises a plasmonic sphere, having a radiusdefining a characteristic size L₂ for the second resonator structure.18. The energy transfer system of claim 6, and said second resonatorstructure comprises a polaritonic sphere, having a radius defining acharacteristic size L₂ for the second resonator structure.
 19. Theenergy transfer device of claim 6, and said second resonator structurecomprises a capacitively-loaded conducting-wire loop, where the radiusof the loop defines a characteristic size L₂ for the second resonatorstructure.
 20. The method of claim 1, wherein the rate of energytransfer from said first resonator structure to said second resonatorstructure is denoted by κ, and wherein the resonator structures aredesigned to have Q₁ and Q₂ satisfy κ/√{square root over (Γ₁Γ₂)}>0.2. 21.The method of claim 20, wherein κ/sqrt(Γ₁*Γ₂)>0.5.
 22. The method ofclaim 21, wherein the second resonator structure has a characteristicsize L₂ and D/L₂>1.
 23. The method of claim 22, wherein D/L₂>3.
 24. Themethod of claim 23 wherein D/L₂>5.
 25. The method of claim 20, whereinκ/sqrt(Γ₁*Γ₂)>1.
 26. The method of claim 25, wherein the secondresonator structure has a characteristic size L₂ and D/L₂>1.
 27. Themethod of claim 26, wherein D/L₂>3.
 28. The method of claim 27 whereinD/L₂>5.
 29. The method of claim 20, wherein κ/sqrt(Γ₁*Γ₂)>5.
 30. Themethod of claim 29, wherein the second resonator structure has acharacteristic size L₂ and D/L₂>1.
 31. The method of claim 30, whereinD/L₂>3.
 32. The method of claim 31 wherein D/L₂>5.
 33. The method ofclaim 3, wherein the rate of energy transfer from said first resonatorstructure to said second resonator structure is denoted by κ, andwherein the resonator structures are designed to have Q₁ and Q₂ satisfyκ/sqrt(Γ₁*Γ₂)>0.5.
 34. The method of claim 33, wherein the secondresonator structure has a characteristic size L₂ and D/L₂>1.
 35. Themethod of claim 34, wherein D/L₂>3.
 36. The method of claim 35, whereinD/L₂>5.
 37. The method of claim 3, wherein the rate of energy transferfrom said first resonator structure to said second resonator structureis denoted by κ, and wherein the resonator structures are designed tohave Q₁ and Q₂ satisfy κ/sqrt(Γ₁*Γ₂)>1.
 38. The method of claim 37,wherein the second resonator structure has a characteristic size L₂ andD/L₂>1.
 39. The method of claim 38, wherein D/L₂>3.
 40. The method ofclaim 39, wherein D/L₂>5.
 41. The system of claim 6, wherein the rate ofenergy transfer from said first resonator structure to said secondresonator structure is denoted by κ, and wherein the resonatorstructures are designed to have Q₁ and Q₂ satisfy κ/sqrt(Γ1*Γ2)>0.2. 42.The system of claim 41, wherein the second resonator structure has acharacteristic size L₂ and D/L₂>1.
 43. The system of claim 42, whereinD/L₂>3.
 44. The system of claim 43, wherein D/L₂>5.
 45. The system ofclaim 6, wherein the rate of energy transfer from said first resonatorstructure to said second resonator structure is denoted by κ, andwherein the resonator structures are designed to have Q₁ and Q₂ satisfyκ/sqrt(Γ₁*Γ₂)>0.5.
 46. The system of claim 45, wherein the secondresonator structure has a characteristic size L₂ and D/L₂>1.
 47. Thesystem of claim 46, wherein D/L₂>3.
 48. The system of claim 47, whereinD/L₂>5.
 49. The system of claim 6, wherein the rate of energy transferfrom said first resonator structure to said second resonator structureis denoted by κ, and wherein the resonator structures are designed tohave Q₁ and Q₂ satisfy κ/sqrt(Γ₁*Γ₂)>1.
 50. The system of claim 49,wherein the second resonator structure has a characteristic size L₂ andD/L₂>1.
 51. The system of claim 50, wherein D/L₂>3.
 52. The system ofclaim 51, wherein, D/L₂>5.
 53. The system of claim 7, wherein the rateof energy transfer from said first resonator structure to said secondresonator structure is denoted by κ, and wherein the resonatorstructures are designed to have Q₁ and Q₂ satisfy κ/sqrt(Γ1*Γ2)>0.2. 54.The system of claim 53, wherein the second resonator structure has acharacteristic size L₂ and D/L₂>1.
 55. The system of claim 54, whereinD/L₂>3.
 56. The system of claim 55, wherein D/L₂>5.
 57. The system ofclaim 6, wherein Q₁>500, and Q₂>500.
 58. The method of claim 1, whereinthe first and second resonator structures are movable relative to oneanother.
 59. The system of claim 6, wherein the first and secondresonator structures are movable relative to one another.
 60. The systemof claim 6, wherein the two said frequencies ω₁ and ω₂ are close towithin the narrower of the two resonance widths Γ₁, and Γ₂.
 61. Themethod of claim 1, wherein D>1 cm.
 62. The method of claim 1, whereinD>30 cm.
 63. The method of claim 1, wherein D>1 m.
 64. The system ofclaim 6, wherein D>1 cm.
 65. The system of claim 6, wherein D>30 cm. 66.The system of claim 6, wherein D>1 m.
 67. The method of claim 1, whereinthe first resonator structure has a characteristic size L₁ and thesecond resonator structure has a characteristic size L₂, and D/L₁>1 andD/L₂>1.
 68. The system of claim 6, wherein the first resonator structurehas a characteristic size L₁ and the second resonator structure has acharacteristic size L₂, and D/L₁>1 and D/L₂>1.
 69. The method of claim1, further comprising applying a feedback mechanism to at least one ofthe resonator structures to correct for detuning of its resonantfrequency.
 70. The system of claim 6, further comprising a feedbackmechanism coupled to at least one of the resonator structures to correctfor detuning of its resonant frequency.